A method for adjusting the path of a satellite to limit a risk of collision with items of debris each having a date of closest pass with the satellite is disclosed including: propagating at least one orbit from the reference path of the satellite according to at least one manoeuvre to the farthest date of closest pass; determining a probability of collision for each item of debris according to the at least one orbit; determining at least one overall probability according to the set of probabilities determined; selecting the lowest overall probability from among the at least one overall probability obtained; determining a command for the satellite including the manoeuvre associated with the lowest overall probability.
PROCÉDÉ D'AJUSTEMENT DE TRAJECTOIRE ORBITALE DE SATELLITE
METHOD FOR ADJUSTING THE ORBITAL PATH OF A SATELLITE
VERFAHREN ZUR EINSTELLUNG DER UMLAUFBAHN EINES SATELLITEN
2023-10-25
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
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